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GB201815274D0 - A wing assembly - Google Patents

A wing assembly

Info

Publication number
GB201815274D0
GB201815274D0 GBGB1815274.4A GB201815274A GB201815274D0 GB 201815274 D0 GB201815274 D0 GB 201815274D0 GB 201815274 A GB201815274 A GB 201815274A GB 201815274 D0 GB201815274 D0 GB 201815274D0
Authority
GB
United Kingdom
Prior art keywords
wing assembly
wing
assembly
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
GBGB1815274.4A
Other versions
GB2577279A (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations Ltd
Original Assignee
Airbus Operations Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations Ltd filed Critical Airbus Operations Ltd
Priority to GB1815274.4A priority Critical patent/GB2577279A/en
Publication of GB201815274D0 publication Critical patent/GB201815274D0/en
Priority to CN201910875854.7A priority patent/CN110920859A/en
Priority to US16/572,968 priority patent/US11370525B2/en
Priority to ES19198076T priority patent/ES2980217T3/en
Priority to EP19198076.2A priority patent/EP3626605B1/en
Publication of GB2577279A publication Critical patent/GB2577279A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/28Leading or trailing edges attached to primary structures, e.g. forming fixed slots
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/26Attaching the wing or tail units or stabilising surfaces
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/187Ribs
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/26Construction, shape, or attachment of separate skins, e.g. panels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10Manufacturing or assembling aircraft, e.g. jigs therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B39/00Locking of screws, bolts or nuts

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Connection Of Plates (AREA)
GB1815274.4A 2018-09-19 2018-09-19 A wing assembly Withdrawn GB2577279A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
GB1815274.4A GB2577279A (en) 2018-09-19 2018-09-19 A wing assembly
CN201910875854.7A CN110920859A (en) 2018-09-19 2019-09-17 Wing assembly
US16/572,968 US11370525B2 (en) 2018-09-19 2019-09-17 Wing assembly tension joint and method of assembly
ES19198076T ES2980217T3 (en) 2018-09-19 2019-09-18 A set of wing
EP19198076.2A EP3626605B1 (en) 2018-09-19 2019-09-18 A wing assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1815274.4A GB2577279A (en) 2018-09-19 2018-09-19 A wing assembly

Publications (2)

Publication Number Publication Date
GB201815274D0 true GB201815274D0 (en) 2018-10-31
GB2577279A GB2577279A (en) 2020-03-25

Family

ID=64013150

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1815274.4A Withdrawn GB2577279A (en) 2018-09-19 2018-09-19 A wing assembly

Country Status (5)

Country Link
US (1) US11370525B2 (en)
EP (1) EP3626605B1 (en)
CN (1) CN110920859A (en)
ES (1) ES2980217T3 (en)
GB (1) GB2577279A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2574391A (en) * 2018-05-31 2019-12-11 Airbus Operations Ltd An aircraft wing and wing tip device
GB2577540A (en) * 2018-09-28 2020-04-01 Airbus Operations Ltd Joint for connecting aircraft structures
CN117842342B (en) * 2024-03-06 2024-05-14 四川迅联达智能科技有限公司 Outer surface conformal system of fixed wing aircraft and aircraft

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3096826A (en) * 1961-08-07 1963-07-09 Hughes Tool Co Rotor blade for rotary-winged aircraft
US5039032A (en) * 1988-11-07 1991-08-13 The Boeing Company High taper wing tip extension
BE1012781A3 (en) * 1999-07-09 2001-03-06 Sonaca Sa Assembly method of a panel on flexible structure open and installation for implementing the method.
GB0805963D0 (en) * 2008-04-02 2008-05-07 Airbus Uk Ltd Aircraft structure
US7975965B2 (en) 2008-05-13 2011-07-12 The Boeing Company Wing tip joint in airfoils
CN201395244Y (en) * 2009-06-04 2010-02-03 中国航空工业集团公司西安飞机设计研究所 Aircraft leading edge slat sealing structure
GB201105104D0 (en) 2011-03-28 2011-05-11 Airbus Operations Ltd Joint
GB201110973D0 (en) * 2011-06-28 2011-08-10 Airbus Operations Ltd Bracket
GB201120707D0 (en) * 2011-12-01 2012-01-11 Airbus Operations Ltd Leading edge structure
GB201120992D0 (en) * 2011-12-07 2012-01-18 Airbus Uk Ltd Aircraft rib assembly
US9056376B2 (en) * 2012-10-29 2015-06-16 The Boeing Company Apparatus and method for remote fastener installation
DE102015105298B4 (en) * 2015-04-08 2021-12-23 Deutsches Zentrum für Luft- und Raumfahrt e.V. Wing structure for flying objects and method for replacing a leading edge of a wing in a wing structure
GB2550175A (en) * 2016-05-11 2017-11-15 Airbus Operations Ltd Aircraft joint
GB2557274A (en) * 2016-12-02 2018-06-20 Airbus Operations Ltd Aerofoil structure components
GB201710385D0 (en) * 2017-06-29 2017-08-16 Airbus Operations Gmbh Aerofoil structure and method of assembly

Also Published As

Publication number Publication date
CN110920859A (en) 2020-03-27
EP3626605A1 (en) 2020-03-25
US20200140059A1 (en) 2020-05-07
EP3626605B1 (en) 2024-03-20
US11370525B2 (en) 2022-06-28
ES2980217T3 (en) 2024-09-30
GB2577279A (en) 2020-03-25

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)